Number |
2016-0141 |
Issued by |
Europe |
Issue date |
2016-07-20 |
Effective date |
2016-08-01 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 700
-
768-60
-
772-60
-
772B-60
-
772C-60
|
Revision |
Not applicable
|
Correction |
This AD is republished to correct the Reason, and an omission in Table 1 of this AD.
|
Supersedure |
This AD supersedes EASA AD 2014-0031 dated 04 February 2014.
|
Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-G702 dated 23 May 2011.
Rolls-Royce NMSB RB.211-72-G872 dated 2 April 2012, or Revision 1 dated 2 July 2012, or Revision 2 dated 08 March 2013.
Rolls-Royce NMSB RB.211-72-H311 dated 08 March 2013.
Rolls-Royce NMSB RB.211-72-AH465 dated 15 July 2013, or Revision 1 dated 10 July 2015, or Revision 2 dated 11 May 2016.
RR Trent 700 EM E-Trent-1RR.
RR Trent 700 TLM T-Trent-1RR.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
16-075 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 19 May 2016 as PAD 16-075 for consultation until 16 June 2016. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|